CN112313147A - 飞行器减阻系统和内部冷却电动马达系统及使用它们的飞行器 - Google Patents
飞行器减阻系统和内部冷却电动马达系统及使用它们的飞行器 Download PDFInfo
- Publication number
- CN112313147A CN112313147A CN201980032466.0A CN201980032466A CN112313147A CN 112313147 A CN112313147 A CN 112313147A CN 201980032466 A CN201980032466 A CN 201980032466A CN 112313147 A CN112313147 A CN 112313147A
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- aircraft
- nacelle
- air
- rotor
- motor
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- 239000012809 cooling fluid Substances 0.000 claims 2
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- 239000007788 liquid Substances 0.000 abstract description 19
- 239000002826 coolant Substances 0.000 abstract description 8
- 230000007246 mechanism Effects 0.000 description 25
- 238000001816 cooling Methods 0.000 description 19
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Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/38—Constructions adapted to reduce effects of aerodynamic or other external heating
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D29/00—Power-plant nacelles, fairings, or cowlings
- B64D29/02—Power-plant nacelles, fairings, or cowlings associated with wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
- B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
- B64C21/08—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like adjustable
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2230/00—Boundary layer controls
- B64C2230/04—Boundary layer controls by actively generating fluid flow
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0226—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising boundary layer control means
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Wind Motors (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Motor Or Generator Cooling System (AREA)
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201862643763P | 2018-03-16 | 2018-03-16 | |
US62/643,763 | 2018-03-16 | ||
US201862694910P | 2018-07-06 | 2018-07-06 | |
US62/694,910 | 2018-07-06 | ||
PCT/US2019/022651 WO2020033010A2 (en) | 2018-03-16 | 2019-03-16 | Aircraft drag reduction system and internally cooled electric motor system and aircraft using same |
Publications (1)
Publication Number | Publication Date |
---|---|
CN112313147A true CN112313147A (zh) | 2021-02-02 |
Family
ID=68290934
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201980032466.0A Pending CN112313147A (zh) | 2018-03-16 | 2019-03-16 | 飞行器减阻系统和内部冷却电动马达系统及使用它们的飞行器 |
Country Status (5)
Country | Link |
---|---|
US (3) | US11161589B2 (de) |
EP (1) | EP3765361A4 (de) |
JP (2) | JP7333144B2 (de) |
CN (1) | CN112313147A (de) |
WO (1) | WO2020033010A2 (de) |
Families Citing this family (20)
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US10900990B2 (en) * | 2019-03-21 | 2021-01-26 | Rosemount Aerospace Inc. | Acoustic air data sensing systems with skin friction sensors |
GB2587670A (en) * | 2019-10-02 | 2021-04-07 | Advanced Mobility Res And Development Ltd | Systems and methods for aircraft |
WO2021112940A1 (en) * | 2019-12-04 | 2021-06-10 | Beta Air, Llc | An integrated electric propulsion assembly |
US11613368B2 (en) * | 2020-01-28 | 2023-03-28 | Rolls-Royce Corporation | Aircraft with electrical energy storage in nacelles |
WO2021157736A1 (en) * | 2020-02-06 | 2021-08-12 | Hapsmobile Inc. | Aerodynamic electric motor nacelle |
US20230074332A1 (en) * | 2020-02-21 | 2023-03-09 | Eaton Intelligent Power Limited | Integrated electric motor and thermal management system |
US11472544B2 (en) * | 2020-03-04 | 2022-10-18 | Textron Innovations Inc. | Electric drive system line replaceable unit with integrated collective actuation |
US11565803B2 (en) | 2020-03-04 | 2023-01-31 | Textron Innovations Inc. | Electric drive system line replaceable unit with integrated cyclic actuation |
CN111348062A (zh) * | 2020-03-21 | 2020-06-30 | 东莞理工学院 | 流体中高速移动物体降低阻力结构 |
US11831220B2 (en) | 2020-06-22 | 2023-11-28 | Textron Innovations Inc. | Electric motor stack with integral one-piece gearbox input shaft |
US11390395B2 (en) * | 2020-06-25 | 2022-07-19 | Textron Innovations Inc. | Aircraft rotor assembly with segmented input shaft for electric motor stack and gearbox unit |
US11781544B2 (en) * | 2020-10-20 | 2023-10-10 | Textron Innovations Inc. | Electric drive system for rotorcraft |
WO2022133486A1 (en) | 2020-12-18 | 2022-06-23 | Joby Aero, Inc. | Electric motor comprising a liquid cooling of wound stator |
US11814163B2 (en) | 2021-01-13 | 2023-11-14 | Textron Innovations Inc. | Electric tiltrotor aircraft with tilting coaxial motors and gearbox |
JP2024506334A (ja) * | 2021-02-09 | 2024-02-13 | ジョビー エアロ,インコーポレイテッド | 航空機推進ユニット |
WO2023041928A1 (en) * | 2021-09-16 | 2023-03-23 | Qdot Technology Ltd | Integrated fan and battery propulsion system |
CN114194403B (zh) * | 2022-01-25 | 2023-06-02 | 广东汇天航空航天科技有限公司 | 驱动装置的散热结构及飞行器 |
EP4253251A1 (de) * | 2022-03-28 | 2023-10-04 | Lilium eAircraft GmbH | Elektrisch angetriebene antriebseinheit eines luftfahrzeuges, luftfahrzeug und steuerverfahren für eine elektrisch angetriebene antriebseinheit |
KR102613732B1 (ko) * | 2022-05-30 | 2023-12-14 | 주식회사 플라나 | 열교환기 및 이를 포함하는 비행기 |
US11679872B1 (en) * | 2022-12-12 | 2023-06-20 | Archer Aviation Inc. | Tilter motor cooling apparatus for vertical takeoff and landing aircraft and operating method of the same |
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JPS63289229A (ja) * | 1987-05-06 | 1988-11-25 | エムテーウー・モートレン‐ウント・ツルビーネン‐ウニオン・ミュンヘン・ゲーエムベーハー | プロップ・ファン・ターボ駆動装置 |
US20130265848A1 (en) * | 2010-06-01 | 2013-10-10 | Esg Mbh | Duct having flow conducting surfaces |
WO2015004370A1 (fr) * | 2013-07-12 | 2015-01-15 | Hutchinson | Dispositif de sustentation à soufflante(s) axiale(s), et aerodyne equipé d'un tel dispositif |
EP2913269A1 (de) * | 2014-02-28 | 2015-09-02 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Drehflügler mit mindestens einem Hauptrotor und mindestens einem Rotor zum Drehmomentausgleich |
US9701399B1 (en) * | 2013-03-18 | 2017-07-11 | Techdyne Llc | Parasitic drag induced boundary layer reduction system and method |
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-
2019
- 2019-03-16 WO PCT/US2019/022651 patent/WO2020033010A2/en active Application Filing
- 2019-03-16 US US16/355,742 patent/US11161589B2/en active Active
- 2019-03-16 EP EP19848482.6A patent/EP3765361A4/de active Pending
- 2019-03-16 JP JP2020547086A patent/JP7333144B2/ja active Active
- 2019-03-16 CN CN201980032466.0A patent/CN112313147A/zh active Pending
- 2019-03-16 US US16/355,745 patent/US11312471B2/en active Active
-
2022
- 2022-01-28 US US17/586,801 patent/US11912393B2/en active Active
-
2023
- 2023-08-11 JP JP2023131709A patent/JP2023159233A/ja active Pending
Patent Citations (5)
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JPS63289229A (ja) * | 1987-05-06 | 1988-11-25 | エムテーウー・モートレン‐ウント・ツルビーネン‐ウニオン・ミュンヘン・ゲーエムベーハー | プロップ・ファン・ターボ駆動装置 |
US20130265848A1 (en) * | 2010-06-01 | 2013-10-10 | Esg Mbh | Duct having flow conducting surfaces |
US9701399B1 (en) * | 2013-03-18 | 2017-07-11 | Techdyne Llc | Parasitic drag induced boundary layer reduction system and method |
WO2015004370A1 (fr) * | 2013-07-12 | 2015-01-15 | Hutchinson | Dispositif de sustentation à soufflante(s) axiale(s), et aerodyne equipé d'un tel dispositif |
EP2913269A1 (de) * | 2014-02-28 | 2015-09-02 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Drehflügler mit mindestens einem Hauptrotor und mindestens einem Rotor zum Drehmomentausgleich |
Also Published As
Publication number | Publication date |
---|---|
EP3765361A4 (de) | 2021-12-08 |
JP2023159233A (ja) | 2023-10-31 |
US20190329858A1 (en) | 2019-10-31 |
WO2020033010A3 (en) | 2020-05-22 |
US11312471B2 (en) | 2022-04-26 |
US11161589B2 (en) | 2021-11-02 |
JP7333144B2 (ja) | 2023-08-24 |
WO2020033010A2 (en) | 2020-02-13 |
US20220169362A1 (en) | 2022-06-02 |
EP3765361A2 (de) | 2021-01-20 |
US20190329859A1 (en) | 2019-10-31 |
JP2021515726A (ja) | 2021-06-24 |
US11912393B2 (en) | 2024-02-27 |
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